Propulsion — Space Hardware Marketplace

AF-M315E (ASCENT) Green Monopropellant

• AppearanceTranslucent, light pink-orange liquid
• Specific gravity1.46
• Freezing pointDoes not freeze; glasses at -80°C

HAN-based green liquid monopropellant, higher performance and lower toxicity than hydrazine, used in NASA GPIM.

Sunbird — Nuclear Fusion Propulsion System

Pulsar Fusion's Sunbird is a Dual Direct Fusion Drive (DDFD) using deuterium + helium-3 fusion: targeting 10,000–15,000 s…

Orbital Arc Thruster and PPU

An ultra-low-mass electric propulsion thruster and power processing unit (PPU) combo for a 2 kW system, offering very…

ND-50 Neumann Drive — Pulsed Cathodic Arc Thruster

Neumann Space's ND-50 is a solid-metal-propellant pulsed cathodic arc thruster: 50 W max power, 1,400–2,000 s Isp, 1.4…

E-2 liquid rocket engine

• ProductOrbiter orbital transfer vehicle
• ParentVAST
• ServiceLast-mile satellite delivery, hosted payloads

The E-2 is a LOX/Kerosene oxidizer-rich staged combustion engine designed for small launch vehicles, aiming to be the…

Herik Labs HL-1 Green Hydrogen Rocket Engine

• PropellantGreen hydrogen
• EmissionsZero greenhouse gas during operation
• ManufacturingMetal 3D printing

Australian green hydrogen rocket engine — 25% higher Isp than alternatives, metal 3D-printed with 85% fewer parts, fully…

Thrusters for very small satellites (Engines for ultra-small spacecraft)

• TypeMicro-propulsion engine
• Target platformCubeSat, microsatellite
• Thrust modeSingle-pulse high-thrust, continuous, or combined

A family of propulsion systems for femto-class and pico-class spacecraft, including ChipSats, designed for single-pulse orbital maneuvers using…

H2/O2 Aerospike Thruster

• PropellantsH2/O2 (from water electrolysis)
• Nozzle typeAerospike
• EmissionsZero carbon (water only byproduct)

Low-thrust hydrogen/oxygen aerospike thruster using water electrolysis, producing zero carbon emissions with water as the only byproduct.

RD-107A Rocket Engine

LOX/kerosene four-chamber booster engine powering Soyuz-2 launch vehicle lateral strap-on boosters, with 1,020 kN vacuum thrust.

NK-15 Rocket Engine

First-stage LOX/kerosene rocket engine of the Soviet N1 Moon rocket, predecessor to NK-33 with 1,510 kN sea-level thrust.

NK-33 Rocket Engine

High-performance LOX/RP-1 staged-combustion rocket engine with 1,510 kN thrust and 137:1 thrust-to-weight ratio, originally developed for Soviet N1…

Green Mobility Module (GMM)

3U, 5 kg non-autonomous electrodynamic-tether module for smallsat deorbit and reboost.

Paladin

• Thrust1 mN
• Thrust (2)15 mN
• Thrust (3)40 mN

Paladin is a pulsed plasma propulsion system that uses solid metal propellants to generate high-velocity plasma for satellite…

Warlock

The Magdrive Warlock is a compact electric propulsion system for CubeSats, utilizing a metal propellant and pulsed power…

Rogue

The Magdrive Rogue is an integrated electric propulsion system for 2U CubeSats, utilizing a metal propellant and pulsed…

Micropropulsion

• TypeMicromachined microthrusters
• IntegrationEmbedded in modular miniaturized modules
• ArrangementCan be arranged in any corner of a nanosatellite

Micropropulsion is a system of micromachined microthrusters embedded in modular miniaturized modules designed for nanosatellites.

HIP_11 Propulsion System

Advanced green hypergolic H2O2 + ionic liquid multi-mode propulsion, up to 310 s Isp, 20-200 N.

HyNOx Propulsion Systems

A customizable propulsion system family built around ISPTech's HyNOx thrusters, tanks and a proprietary control unit, tailored to…